Structural reinforcement system for automotive vehicles

ABSTRACT

The invention relates to a new method and a new apparatus to accurately measure flow rates in injection systems such as gasoline, direct injection gasoline and diesel downstream of the injector where the fuel (liquid in general) is discharged from a nozzle (e.g. an injector). More specifically, it measures the flow velocities and volumetric flow rates in highly transient flows discharged cyclically with injection duration within a few hundred microseconds. Moreover, it is able to resolve multiple injection shots produced within an engine cycle with high volumetric (0.01 mm3) and temporal (10 μs) sensitivities. The main uses of this instrument in automotive industry are manufactures of FIE, injection test machines and injection diagnostic systems. In other industries the uses maybe represented by measuring and controlling of highly transient flows with a need to accurately perform quantitative flow data in wide range of timing and dosing.

CLAIM OF PRIORITY

This application claims the benefit of U.S. provisional application Nos.60/650,347, filed Feb. 4, 2005 and 60/______, (Attorney Docket No.1204.002P2), filed Feb. 1, 2006, both of which are here by incorporatedby reference.

FIELD OF THE INVENTION

The present invention relates to apparatuses and methods for measuringquantities of flowing fluids, and more particularly, to an improved flowmeter and methods of using the flow meter.

BACKGROUND OF THE INVENTION

In the automotive field, fuel injection equipment (FIE) needs to bequantitatively tested in terms of timing of injection events andinjection volume; sometimes called dosing. For diesel engines, therequirements of temporal resolution and dosing accuracy are increasedbecause of multiple injections per cycle are used to increase fuelefficiency and to reduce emissions, especially soot and NOx.

Known FIE testing equipment is limited to injection volumes that rangeonly over an order of magnitude; e.g. about 10 mm3 to about 100 mm3.Moreover, known FIE testing equipment lacks the resolution todistinguish between injection events that occur in diesel engines.Lastly, known FIE testing equipment is costly meaning that it may not beavailable to small companies, creating a barrier to entering the marketof providing testing services.

The present invention overcomes one or more of these drawbacks.

SUMMARY OF THE INVENTION

The invention relates to a new method and a new apparatus to accuratelymeasure flow rates in injection systems such as gasoline, directinjection gasoline and diesel downstream of the injector where the fuel(liquid in general) is discharged from a nozzle (e.g. an injector). Morespecifically, it measures the flow velocities and volumetric flow ratesin highly transient flows discharged cyclically with injection durationwithin a few hundred microseconds. Moreover, it is able to resolvemultiple injection shots produced within an engine cycle with highvolumetric (0.01 mm3) and temporal (10 μs) sensitivities. The main usesof this instrument in automotive industry are manufactures of FIE,injection test machines and injection diagnostic systems. In otherindustries the uses maybe represented by measuring and controlling ofhighly transient flows with a need to accurately perform quantitativeflow data in wide range of timing and dosing.

BRIEF DESCRIPTION OF THE DRAWINGS

In the drawings:

FIG. 1 depicts schematically one embodiment of a flow meter comprisingtwo sensor sets, with each set have a pair of sensors.

FIG. 2 depicts a flow chart of the method of one embodiment of theinvention.

DETAILED DESCRIPTION

The present invention comprises a flow meter having at least one conduitthrough which a fluid can flow. The conduit generally has a circularcross-section, although other cross sections are also suitable (e.g.oval). The length of the conduit is not particularly critical, althoughlengths shorter than about 1 foot are preferred with a length of lessabout than 6 inches being most preferred. Although use of a singleconduit is preferred, several conduits may be used in conjunction witheach other to form a flow meter.

The flow meter of the present invention is suitable for analyzing a widerange of fluids, but finds a particular application in the automotivearea, and in particular, for analyzing the flow of fuels. For example,fuel injectors for automotive engines may be connected to the flow meterto determine the amount of fuel emitted by the injector. The flow metergenerally measures the propagation of the fluid down the conduit bydetecting the fluid or a changing physical characteristic as each sensor(e.g. the pressure exerted by the fluid). Because of high pressure andshort injection event like those common in fuel injectors, the pressurewave will be substantially flat, meaning that fluid near the center ofthe conduit is moving at nearly the same rate as fluid near the conduitwall.

Each conduit of the flow meter includes a measure section 10 as shownschematically in FIG. 1, comprising at least two sensors 12, 14 andpreferably more sensors such as three, four, five or more sensors. Thesensors are spaced from each other longitudinally along the length ofthe conduit. Any two sensors may be considered a sensor pair such as thefirst and second sensors in the conduit or the first and fourth, etc.,with sensors numbered from upstream to downstream. Each sensor isdesigned to detect the presence of fluid in the conduit. Alternately,the sensor is used to detect a property of a fluid in the conduit thatmay indicate presence of the fluid in the conduit. For example, apressure sensor may sense a change in fluid pressure or a temperaturesensor may sense a change in temperature of the fluid. Preferably, aconduit comprises at least two pressure sensors. Sensors that have thesefunctionalities may include sensors made by any suitable manufacturingtechnique (e.g. MEMS). Although not required, the sensors of a givensensor pair should be the same type e.g. both pressure sensors.

The sensors are placed so as not to obstruct in the fluid flow. Forexample, the sensors may be housed in the wall of the conduit with anopening to the conduit providing the sensor with access to the fluid.This arrangement of sensors provides no obstruction of the fluid flow bythe sensor and thus minimal interference and more accurate measurements.In another embodiment, a housing is placed around the conduit as asupport mechanism for the sensors, which are placed in the housing afteran access hole has been made in the conduit. In one aspect the housingis adhesively bonded, clamped or both to the conduit.

Moreover, the sensors may also be angularly offset. The shift anglewould be used to reduce or eliminate effects of micro-vortices that maybe created in the flowing fluid due to interaction with upstreamsensors. This feature is optional, and while a single offset angle ispreferably selected for a conduit or flow meter, this is not necessarilythe case.

In addition to the measurement section, the conduit further comprises anoutlet down stream from the measurement section. The outlet comprises avariable orifice. The variable orifice permits the back pressure createdby the flowing fluid to be adjusted. Back pressure is used to reduceturbulence in the conduit. The adjustment to the orifice may be manual(e.g. by the operator of the flow meter) or automatic (e.g. by a dataprocessing unit of the flow meter).

In addition to the conduit, the flow meter further comprises anappropriately programmed data processing unit that receives signals fromthe sensor in the measurement section. The data processing unit may sendsignals to the sensors or the outlet to alter the functionality of thesecomponents.

The data processing unit may include a variety of functionalitiesincluding signal processing units, central processing units, dataacquisition units, graphic processing units, memory, storage, outputdevice (e.g. displays or printers), input devices (e.g. keyboards, mice,or the like), or the like and combinations thereof. Signal processingunits may include the use of one or more filters (e.g. Kalman filters).The data processing unit may comprise a general purpose computer (e.g. adesktop or laptop), as these would have sufficient computing power tomake any necessary calculations in a negligible amount of the time (e.g.less than about 10 sec).

The programming for the data processing unit includes instructions tocarry out calculations using inputs from the sensors as discussed below.The flow velocity of the fluid at any sensor location can be calculatedat any distance from the centerline of the conduit. Also, the volumetricflow rate across the cross section of the conduit can be calculated atany sensor location.

The flow meter discussed above is utilized to carry out the methods ofthe present invention including calculating the flow velocity andvolumetric flow rate of an automotive fluid, and automotive fuels suchas gasoline diesel, bio-diesel, ethanol, and combinations thereof.

Calculating the flow velocity and flow rate comprise measuring thepropagation of pressure wave through the conduit. The existence of thepressure wave, as well as the intensity of the pressure wave, is used asinputs for the calculations.

Calculating the velocity and flow rate comprises calculating a pressuregradient in the conduit and using the pressure gradient information asinputs for the velocity and flow rate calculation.

At least two methods exist for calculating the pressure gradient fromthe signals generated by the pressure sensors. In the direct method, thepressures exerted by the pressure wave are measured by two or moresensors. For two sensors, the pressure signals are converted to thepressure gradient signal by dividing the difference in the pressuresignals by the distance between the sensors (z₁₂): $\begin{matrix}{\frac{\delta\quad P}{\delta\quad z} \cong \frac{{P_{2}(t)} - {P_{1}(t)}}{z_{12}}} & {{eq}.\quad 1}\end{matrix}$

In the time of flight method, the time it takes the pressure wave totravel from one sensor to the other is noted by the sensors to give timeτ₁₂. Time τ₁₂ may be calculated using a spectral method, a timecorrelation method or the like. The speed of sound (V_(sound)) in thefluid is calculated by z₁₂/τ₁₂. Using this information, for these andother sensors in the conduit, using only a single sensor, a pressuregradient can be calculated. A virtual displacement technique is used,meaning that a hypothetical second sensor is paired with each sensor,with the hypothetical sensor displaced from the first sensor by adistance d. Any distance d may be used; however, the smaller thedistance, the more precise the calculation. The pressure gradient iscalculated according to this equation: $\begin{matrix}{\frac{\delta\quad P}{\delta\quad z} \cong \frac{{P_{i}(t)} - {P_{i}\left( {t - \frac{d}{V_{sound}}} \right)}}{d}} & {{eq}\quad.\quad 2}\end{matrix}$

Through this method a single sensor can be used to calculate thepressure gradient at any particular location within the conduit, thusincreasing the number of data points, thus improving accuracy andresolution.

Spline and/or bandlimited interpolation techniques may be used toimprove the resolution of the data and particularly the time data toincrease the resolution and/or accuracy of either technique.

The pressure gradient spectra can be represented by it Fourier Seriescomponents, K_(n): $\begin{matrix}{\frac{\delta\quad P}{\delta\quad z} = {\sum\limits_{n = {- \infty}}^{\infty}\quad{K_{n}{\mathbb{e}}^{{\mathbb{i}}\quad\omega_{n}t}}}} & {{eq}.\quad 3}\end{matrix}$

From the pressure gradient information, the velocity and flow rate ofthe fluid in the conduit can be calculated. In particular, simplifiedNavier-Stokes equations are utilized to provide closed form, analyticalsolutions to the calculations of the flow velocity and flow rate. Thetime dependent flow velocity at any given distance from the centerlineof the conduit is calculated by the following equation: $\begin{matrix}{{V\left( {r,t} \right)} = {\frac{K_{0}{R^{2}\left( {r^{2} - 1} \right)}}{4\quad\mu} + {\sum\limits_{n = 1}^{\infty}\quad{{\frac{K_{n}}{i\quad\omega_{n}\rho}\left\lbrack {\frac{J_{0}\left( {\alpha_{n}i^{3/2}r} \right)}{J_{0}\left( {\alpha_{n}i^{3/2}} \right)} - 1} \right\rbrack}{\mathbb{e}}^{{\mathbb{i}}\quad\omega_{n}t}}} + {C.C.}}} & {{eq}.\quad 4}\end{matrix}$and the volumetric flow rate is calculated by the follow equation:$\begin{matrix}{{F(t)} = {{- \frac{K_{0}\pi\quad R^{4}}{8\quad\mu}} + {\sum\limits_{n = 1}^{\infty}\quad{{\frac{K_{n}\pi\quad R^{2}}{i\quad\omega_{n}\rho}\left\lbrack {\frac{2{J_{1}\left( {\alpha_{n}i^{3/2}} \right)}}{\alpha_{n}i^{3/2}{J_{0}\left( {\alpha_{n}i^{3/2}} \right)}} - 1} \right\rbrack}{\mathbb{e}}^{{\mathbb{i}}\quad\omega_{n}t}}} + {C.C.}}} & {{eq}.\quad 5}\end{matrix}$wherein R is the radius of the conduit;

-   r is the normalized radius (0=centerline, and 1=R);-   μ is the viscosity of the fluid (ρ*ν);-   ρ is the density of the fluid;-   α_(n) is the Taylor number $R\sqrt{\frac{\omega_{n}}{\nu};}$-   ν is the kinetic viscosity of the fluid;-   J₀( ) and J₁( ) are Bessel functions; and-   C. C. are the complex conjugate terms.

These calculations are closed form solutions for the flow velocity andvolumetric flow of the fluid that do not require iteration.

The results calculated by the above equations may be further processedto improve their accuracy, resolution or to improve the speed ofprocessing. Processing speed may be increased by simplifying the Besselfunction ratios, such as those that appear in the volumetric flow rateequation. For Bessel function ratios such as$\frac{J_{1}\left( {i^{3/2}x} \right)}{J_{0}\left( {i^{3/2}x} \right)},$as values of become larger, the numerator and denominator head towardinfinity while the ratio remains stable. A numerical method of dealingwith a related problem has been suggested in “Evaluation and inversionof the Ratios of Modified Bessel Function” by Geoffery Hill, ACMTransaction on Mathematical Software, Vol. 7, No. 2, Jun. 1981, Pages199-208, hereby incorporated by reference. The relationship betweenmodified Bessel functions and Bessel functions is as follows:I_(n)(x)=i^(−n)J_(n)(ix). Thus, using the suggested fraction expansionsubstituted with the Bessel function (instead of the modified Besselfunctions) leads to the following equation: $\begin{matrix}\begin{matrix}{\frac{J_{1}\left( {i^{3/2}x} \right)}{J_{0}\left( {i^{3/2}x} \right)} = {i\left( {1 - \frac{2}{{4\quad y} - 1 - \frac{1}{{4\quad{y/3}} - 2 - \frac{1}{{4\quad{y/5}} - 2 - \frac{1}{4\quad{y/7}\ldots}}}}} \right)}} \\{where} \\{y = {i^{1/2}x}}\end{matrix} & {{eq}.\quad 6}\end{matrix}$Calculating this to only a few terms (e.g. about 2 to about 10) of theexpansion provides excellent accuracy for the Bessel function ratios ina manner that is rapidly calculated. This also speeds the calculation ofthe volumetric flow rate.

As seen in FIG. 2, in one embodiment of the method comprises calculatingthe pressure gradient from the pressure signals via the direct method,the time of flight method or a combination thereof. From the pressuregradients, pressure gradient spectra are calculated using fast Fouriertransform. The pressure gradient spectra are used as inputs for equation5 to obtain spectra for the volumetric flow rate. Inverse fast Fouriertransform is used to obtain the flow velocity and volumetric flow rate.A similar method is used to achieve the flow velocity.

It will be further appreciated that functions or structures of aplurality of components or steps may be combined into a single componentor step, or the functions or structures of one-step or component may besplit among plural steps or components. The present inventioncontemplates all of these combinations. Unless stated otherwise,dimensions and geometries of the various structures depicted herein arenot intended to be restrictive of the invention, and other dimensions orgeometries are possible. Plural structural components or steps can beprovided by a single integrated structure or step. Alternatively, asingle integrated structure or step might be divided into separateplural components or steps. In addition, while a feature of the presentinvention may have been described in the context of only one of theillustrated embodiments, such feature may be combined with one or moreother features of other embodiments, for any given application. It willalso be appreciated from the above that the fabrication of the uniquestructures herein and the operation thereof also constitute methods inaccordance with the present invention. The present invention alsoencompasses intermediate and end products resulting from the practice ofthe methods herein. The use of “comprising” or “including” alsocontemplates embodiments that “consist essentially of” or “consist of”the recited feature.

The explanations and illustrations presented herein are intended toacquaint others skilled in the art with the invention, its principles,and its practical application. Those skilled in the art may adapt andapply the invention in its numerous forms, as may be best suited to therequirements of a particular use. Accordingly, the specific embodimentsof the present invention as set forth are not intended as beingexhaustive or limiting of the invention. The scope of the inventionshould, therefore, be determined not with reference to the abovedescription, but should instead be determined with reference to theappended claims, along with the full scope of equivalents to which suchclaims are entitled. The disclosures of all articles and references,including patent applications and publications, are incorporated byreference for all purposes.

1. A flow meter, comprising: a conduit comprising at least two pressuresensors longitudinally spaced from each other in the conduit; and a dataprocessing unit connected to the pressure sensors to receive signalsfrom the pressure sensors, wherein the data processing unit isprogrammed to calculate a pressure gradient from the signals receivedfrom the pressure sensors and further programmed to calculate one ormore of flow velocity or volumetric flow rate of a fluid flowing in theconduit using a non-iterative calculation.
 2. The flow meter of claim 1wherein the at least two pressure sensors are placed so as not toobstruct fluid flow in the conduit.
 3. The flow meter of claim 2 whereinthe at least two pressure sensors are placed in the wall of the conduit.4. The flow meter of claim 2 wherein the at least two pressure sensorsare placed in one or more housing on the conduit.
 5. The flow meter ofclaim 2 wherein the at least two pressure sensors are angularly offsetfrom one another.
 6. The flow meter of claim 5 further comprising avariable outlet.
 7. The flow meter of claim 6 further comprising aninjector.
 8. A method metering a flowing fluid, comprising: flowing afluid in a conduit having at least two pressure sensors to generatepressure sensor outputs; calculating one or more pressure gradients fromthe pressure sensors outputs; calculating one or more flow velocities orvolumetric flow rates from the pressure gradients using a closed formsolution.
 9. The method of claim 8 wherein the flow velocity orvolumetric flow rate calculation is non-iterative.
 10. The method ofclaim 9 further comprising interpolating the pressure sensor outputsbefore calculating the one or more pressure gradients.
 11. The method ofclaim 8 wherein calculating the one or more pressure gradients comprisesutilizing the direct method, the time of flight method or a combinationthereof.
 12. The method of claim 11 wherein calculating the flowvelocity is calculated according to equation
 4. 13. The method of claim12 wherein calculating the volumetric flow rate is calculated accordingto equation
 5. 14. The method of claim 8 wherein calculating one or morevolumetric flow rates comprises using equation
 6. 15. The method ofclaim 8 wherein the at least two pressure sensors are angularly offset.16. The method of claim 15 wherein the pressure sensors do not obstructthe flow of fluid in the conduit.
 17. A method metering a flowing fluid,comprising: flowing a fluid in a conduit having at least two pressuresensors to generate pressure sensor outputs, the at least two pressuresensors are angularly offset and do not obstruct the flow of fluid inthe conduit; calculating one or more pressure gradients from thepressure sensors outputs; calculating one or more flow velocities orvolumetric flow rates from the pressure gradients using a closed formsolution, wherein the flow velocity or volumetric flow rate calculationis non-iterative; and interpolating the pressure sensor outputs beforecalculating the one or more pressure gradients, wherein calculating theone or more pressure gradients comprises utilizing the direct method,the time of flight method or a combination thereof.